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Comparison of visualized turbine endwall secondary flows and measured heat transfer patterns
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Russell, L. M. Gaugler, R. E. |
| Copyright Year | 1983 |
| Description | Various flow visualization techniques were used to define the secondary flows near the endwall in a large heat transfer data. A comparison of the visualized flow patterns and the measured Stanton number distribution was made for cases where the inlet Reynolds number and exit Mach number were matched. Flows were visualized by using neutrally buoyant helium-filled soap bubbles, by using smoke from oil soaked cigars, and by a few techniques using permanent marker pen ink dots and synthetic wintergreen oil. Details of the horseshoe vortex and secondary flows can be directly compared with heat transfer distribution. Near the cascade entrance there is an obvious correlation between the two sets of data, but well into the passage the effect of secondary flow is not as obvious. |
| File Size | 2730025 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830006164 |
| Archival Resource Key | ark:/13960/t3mw78981 |
| Language | English |
| Publisher Date | 1983-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Cascade Flow Bubbles Gas Turbines Turbulent Flow Vortices Flow Distribution Flow Visualization Vanes End Plates Secondary Flow Heat Transfer Boundary Layers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |